Polarization Re-alignment for Mobile Satellite Terminals

ABSTRACT

A system for allowing ground terminals, specifically mobile ground terminals, to dynamically and electronically realign signal polarizations to match that of incoming and outgoing signal polarizations from designated space assets, specifically communications from satellites, comprising an adaptive re-orientation technique based on a cost minimization function, and a means of direct calculations of weighting components based on the knowledge of the orientation and bearing of both the satellites and the ground terminals. The embodiment will allow a mobile ground terminal to electronically realign itself to the signals of a satellite, without the need for mechanical processes to physically re-orient the antenna array.

This application is a continuation of application No. 12/847,997, filed on Jul. 30, 2010, now bending.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to the field of wireless communication systems and electronic processing and, in particular, transmission and reception architectures between a radio frequency (RF) receiver and transmitter. More specifically, but without limitation thereto, the present invention pertains to a communications system and method that allows mobile ground terminals, or smart antennas to, dynamically realign itself to the signal polarizations of a designated asset (primarily satellites) utilizing a cost optimization program, reuse frequencies via orthogonal polarization beams, and switch receiving polarizations between circular polarizations (CP) and linear polarizations (LP).

2. Description of Related Art

In wireless communications, satellite to ground terminal communication technologies are currently utilized in two different ways. Fixed Service Satellites (FSS) utilize satellites placed in geostationary orbit (GEO) transmitting and receiving signals from ground terminals that are fixed in position. Direct-to-Home (DTH) satellite dishes that serve to bring satellite-beamed television into private homes are an example of FSS. On the other hand, Mobile Service Satellites (MSS) rely on GEO satellites to transmit and receive signals to and from mobile terminals, such as a Global Positioning System (GPS) receiver in a car, boat, etc.

FSS and MSS are just two methods of wireless communications that utilize polarization diversity, each with differing applications and requirements. Polarization diversity has enabled the same frequency to be reused over the same spectra, allowing one frequency to transmit two or more distinct sets of information. This has proved to be beneficial to both RF communications and RF radar applications. RF transmissions are usually either circularly polarized (CP), or linearly polarized (LP). LP signals can be polarized either vertically (VP) or horizontally (HP). Additionally, CP signals can either be right-hand circularly polarized (RHCP) or left-hand circularly polarized (LHCP).

FSS systems typically employ a LP signals, as the ground receiver (terminal) is fixed, and there is no issue with the signals falling out of phase, interfering with each other, or unable to be received because the ground terminal does not move in relation to the satellite. On the other hand, due to the mobile nature of MSS platforms (such as a truck moving both directionally and spatially to the satellite), a CP signal offers a better option as it offers an omnidirectional radio wave signal that can be received and decoded regardless of the direction or spatial displacement of the terminal. However, there are some DBS (direct broadcast satellites) that utilize CP as well as LP signals.

Because of this, polarization alignment techniques are important on satellite communications to reduce interference due to misalignment of the orientations of transmission signals and received antennas either for large earth station antennas as well as the small aperture antennas found in VSAT (very small aperture terminals) and Direct-to-Home (DTH) services, such as those used for satellite-based television (e.g. DirecTV or Dish Network). Currently, the techniques used for polarization realignment are mechanical-based, using gimbals and tracks to physically rotate and re-orient the ground terminal to the satellite.

While mechanically driving the satellite receiver (also known as the ground terminal) is a practical method of re-orienting the dish to properly receive the RF signals, the gimbals and tracks pose a problem for mobile ground terminals. However, mobile ground terminals are limited in two important ways. The extra machinery necessary for mechanized terminal re-orientation adds unnecessary weight and complexity to these mobile terminals, when their chief aim is simplicity with low cost and weight. This is because these mobile terminals do not have the physical space or power requirements that the FSS systems have.

For the foregoing reasons, there is a need in satellite communications for a system to electronically re-orient, specifically but without limitation thereto, mobile ground terminal receivers to match the polarizations of satellite RF signals, thus removing the requirement of mechanically re-orienting the ground terminals. Furthermore, there is a need to create a system that allows mobile ground terminals to seamlessly switch between polarizations, allowing these mobile ground terminals to receive both circularly polarized RF signals as well as linearly polarized RF signals.

An embodiment of the present invention involves a dynamic improvement of how ground terminals receive RF signals from satellites by utilizing an electronic method of decoding transmitted RF signals from satellites, whether they are circularly polarized or linearly polarized. The proposed architecture will allow ground terminals, in particular mobile VSAT or DTV operators, to use satellite assets either with LP or CP satellites for their services. The ground terminals will dynamically realign itself via electronics, and not physically moving the receiver, to the polarizations of radiation from a targeted satellite.

The following references are presented for further background information:

-   -   1. R. G. Vaughan, J. B. Anderson; “Antenna Diversity in Mobile         Communications;” IEEE Transactions on Vehicular Technology; Nov.         1987; pp. 149-172; and     -   2. R. G. Vaughan; “Polarization Diversity in Mobile         Communications;” IEEE Transactions on Vehicular Technology; Aug.         1990; pp. 177-186; and     -   3. K. Aydin, T. A. Seliga; “Remote Sensing of Hail with a Dual         Linear Polarization Radar;” Journal of Climate and Applied         Meteorology; Oct. 1986; V. 25; pp. 1475-1484; and     -   4. S. Fiedler, F. Fresia, E. Pagana; “Method and System for         Polarization Alignment of an Earth Station Antenna with the         Polarization Axis of a Satellite Antenna;” EU Patent No.         EP1303002; Mar. 9, 2008.

SUMMARY OF THE INVENTION

The present invention provides a dynamic communication system suitable for allowing dynamic signal polarization realignment by ground terminals, specifically but with no limitation thereto, mobile ground terminals, realigning the signals to those of radiated and/or received signals by designated space assets, specifically satellites. These satellites may be in GEO (geostationary earth orbit), LEO (low earth orbit), and MEO (medium earth orbit) as well as in slightly inclined orbits from GEO orbits.

Due to the fact that satellites and mobile ground terminals are constantly in motion, the orientation of polarizations relative to one another between a user terminal and the targeted satellite must be known. Thus, the following information is needed for implementation of the polarization realignment:

-   -   1. Information on current locations and orientations of user         terminals; and     -   2. Information on current orbital slots and orientations of         targeted satellites.

More specifically, the present invention provides a means of electronically realigning polarizations of incoming and outgoing signals for mobile ground terminals via a cost minimization technique (or, an angle optimization process) comprising: a set of inputs, specifically an antenna array, electronically connected to an angle optimization process module, which in turn is connected to an angle rotation process module. This embodiment removes the requirement for a means of mechanically reorienting the ground terminal antenna array for continually matching the space asset's signal polarizations, as the processing for realignment is done electronically.

Accordingly, several advantages of one or more aspects are as follows: to provide a means of electronically realigning a ground terminal to match signal polarizations (regardless of whether they are CP or LP) to that of incoming or outgoing signals by a designated space asset, that do not need a mechanical means of realigning polarizations, and that can seamlessly switch between signal polarizations thus giving ground terminals the ability to communicate with different satellites, thus increasing the flexibility of ground terminals.

BRIEF DESCRIPTIONS OF THE DRAWINGS

The objects, features and advantages of the present invention will become better understood from the following detailed descriptions of the preferred embodiment of the invention in conjunction with reference to the following appended claims, and accompany drawings where:

FIG. 1 shows polarization orientations for both the signals from a targeted satellite and that of a user terminal.

FIG. 2 shows the use of dynamic polarization re-alignment via cost minimization technique.

The 201 is a patch antenna.

The 202 is an amplifier.

The 203 is a frequency down converter.

The 204 is an A/D (analog-to-digital) converter.

The 205 is an Angle optimization process module.

The 206 is an Angle rotation process module.

The 207 is a compass.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

The present invention relates to the fields of communication systems, and in particular, satellite to ground terminal communications. More specifically, but without limitation thereto, the present invention pertains to a communication system and method that dynamically realigns incoming and outgoing signal polarizations for ground terminals to those of designated space assets, specifically satellites.

In order to determine the orientation of polarizations relative to one another between a user terminal and a targeted satellite, the following information is needed for implementation of dynamic polarization realignments:

-   -   1) information on current locations and orientations of user         terminals     -   2) information on current orbital slots and orientations of         targeted satellites.

The relative geometries are illustrated in FIG. 1, assuming both polarizations from satellite and users are LPs. (x,y) are the coordinate for satellite signals, and (x_(tm), y_(tm)) are those for user terminals. For GEO satellites, it is common to orient the E-field of the HP to the “North” when the satellites are in orbit. Therefore, the offset angle, θ, can be roughly determined via an electronic compass on a mobile user terminal. The polarization realignment, with the knowledge of θ, can be achieved via the following equations:

VP=VPtm*cos θ−HPtm sin θ  (1)

HP=VPtm*sin θ+HPtm cos θ  (2)

The accuracy of the offset angle shall be better than ˜±6° to achieve a 20 dB isolation requirement between the two LP signals.

The concept of linear polarization re-orientation to dynamically match polarizations of incoming signals of for mobile terminals with a set of linearly polarized output ports comprising:

-   -   a. direct calculations of weighting components based on         knowledge of orientation of the terminals to a moving platform         and bearing of the platform;     -   b. In order to achieve better isolation, it is possible to use         optimization loop to re-align the polarizations for the mobile         terminals, as indicated in FIG. 2. Described as below:

As indicated in FIG. 2, the antenna array 201 has two orthogonal polarization output ports. Each signal component goes through an amplifier 202, which boosts the strength of the signal. The boosted signal then passes through a frequency down converter 203, then passing to an analog-to-digital (A/D) converter 204 to convert the analog signal into a digital one. Finally, the digital signals then go through an angle optimization process module 205. Here, a process determines the difference of θ between (x,y) and (x_(tm), y_(tm)). After determining the difference of θ, the signals undergo a cost optimization program that determines the cross correlation between the VP and HP. This is compared with the initial θ from an electronic compass 207. Once the new optimal angle (θ) is determined, information is sent to angle rotation process module 206 to electronically reorient antenna array 201 to receive the highest quality signal.

In the angle optimization process module 205, first resolving the mixed signals to VP (vertical polarization) and HP (horizontal) polarization components according to the initial θ provided by compass, then calculating the cost by cross correlation between VP and HP, comparing the cost with a predefined threshold cost. If the cost is greater than the threshold, calculating the cost gradient will result in a new θ. The loop continues until the cost is less than the threshold cost. The final θ will be delivered to the angle rotation process module and output better set of isolated VP and HP, at which point the signal polarizations are matching and the ground terminal will begin decoding the information. 

1-16. (canceled)
 17. A method for angle realignment, comprising: obtaining a first vertical polarization component and a first horizontal polarization component; resolving a second vertical polarization component based on information comprising a polarization offset angle and said first vertical and horizontal polarization components; resolving a second horizontal polarization component based on information comprising said polarization offset angle and said first vertical and horizontal polarization components; calculating a cost based on information comprising a cross correlation between said second vertical and horizontal polarization components; and after said calculating said cost, calculating a cost gradient.
 18. The method of claim 17, wherein said polarization offset angle has an accuracy between +6 degrees and −6 degrees.
 19. The method of claim 17 further comprising said calculating said cost gradient in response to finding said calculated cost is greater than a threshold cost.
 20. The method of claim 17 being performed on a mobile terminal.
 21. The method of claim 17 further comprising determining said polarization offset angle via a compass.
 22. The method of claim 17, wherein said first vertical and horizontal polarization components are converted into ones in a digital mode.
 23. The method of claim 17 further comprising said resolving said second vertical polarization component based on information comprising a combination of said first vertical polarization component multiplied by cosine of said polarization offset angle minus said first horizontal polarization component multiplied by sine of said polarization offset angle.
 24. The method of claim 17 further comprising said resolving said second horizontal polarization component based on information comprising a combination of said first vertical polarization component multiplied by sine of said polarization offset angle plus said first horizontal polarization component multiplied by cosine of said polarization offset angle.
 25. A method for angle realignment, comprising: obtaining a first vertical polarization component and a first horizontal polarization component; resolving a second vertical polarization component based on information comprising a polarization offset angle and said first vertical and horizontal polarization components; resolving a second horizontal polarization component based on information comprising said polarization offset angle and said first vertical and horizontal polarization components; calculating a cost based on information comprising a cross correlation between said second vertical and horizontal polarization components; and after said calculating said cost, performing an angle rotation process to output a third vertical polarization component based on information comprising said polarization offset angle and said first vertical and horizontal polarization components and to output a third horizontal polarization component based on information comprising said polarization offset angle and said first vertical and horizontal polarization components.
 26. The method of claim 25, after said performing said angle rotation process, further comprising performing a decoding process.
 27. The method of claim 25 further comprising said performing said angle rotation process in response to finding said calculated cost is less than a threshold cost.
 28. The method of claim 25 being performed on a movable terminal
 29. The method of claim 25, wherein said third vertical polarization component is associated with a combination of said first vertical polarization component multiplied by cosine of said polarization offset angle minus said first horizontal polarization component multiplied by sine of said polarization offset angle.
 30. The method of claim 25, wherein said third horizontal polarization component is associated with a combination of said first vertical polarization component multiplied by sine of said polarization offset angle plus said first horizontal polarization component multiplied by cosine of said polarization offset angle.
 31. A method for angle realignment, comprising: obtaining a first vertical polarization component and a first horizontal polarization component; resolving a second vertical polarization component based on information comprising a first polarization offset angle and said first vertical and horizontal polarization components; resolving a second horizontal polarization component based on information comprising said polarization offset angle and said first vertical and horizontal polarization components; calculating a first cost based on information comprising a cross correlation between said second vertical and horizontal polarization components; and after said calculating said first cost, calculating a cost gradient; obtaining a second polarization offset angle based on information comprising said cost gradient; resolving a third vertical polarization component based on information comprising said second polarization offset angle and said first vertical and horizontal polarization components; resolving a third horizontal polarization component based on information comprising said second polarization offset angle and said first vertical and horizontal polarization components; calculating a second cost based on information comprising a cross correlation between said third vertical and horizontal polarization components; and after said calculating said cost, performing an angle rotation process to output a fourth vertical polarization component and a fourth horizontal polarization component based on information comprising said second polarization offset angle and said first vertical and horizontal polarization components.
 32. The method of claim 31 further comprising said calculating said cost gradient in response to finding said first cost is greater than a threshold cost.
 33. The method of claim 31 further comprising said performing said angle rotation process in response to finding said second cost is less than a threshold cost.
 34. The method of claim 31 being performed on a mobile terminal.
 35. The method of claim 31, wherein said fourth vertical polarization component is associated with a combination of said first vertical polarization component multiplied by cosine of said second polarization offset angle minus said first horizontal polarization component multiplied by sine of said second polarization offset angle.
 36. The method of claim 31 further comprising said resolving said third vertical polarization component based on information comprising a combination of said first vertical polarization component multiplied by cosine of said second polarization offset angle minus said first horizontal polarization component multiplied by sine of said second polarization offset angle. 